N338NW

Service difficulty reports · 192

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N338NW' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DALA2014110605945Power Supply · inoperativeDURING NON ROUTINE CHECK, FOUND EPSU INOPERATIVE AT 13WL. MAINTENANCE REPLACED EPSU AT 13WL AND FUNCTIONAL CHECK WAS NORMAL.Nov 4, 2014 · N338NW · Airbus A320212 · Emergency LightingSDR DALA2014103105862Access Door · corrodedDURING INSPECTION, FOUND CORROSION ON EXTERNAL SKIN OF ACCESS DOOR 312AR LOCATED BETWEEN FR70-FR73. REPLACED ACCESS DOOR 312AR LOCATED BETWEEN FR 70-FR 73 TAIL CONE IAW SRM 51-72-11.Oct 30, 2014 · N338NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2014103105859Skin · corrodedDURING INSPECTION, FOUND CORROSION ON INNER SKIN LOCATED FWD PAX CABIN ENTRY DOOR AT FR 20, LEVEL STR 23 LT WITH MEASUREMENT OF L=1.026", W=0.832", D=0.002". APPROXIMATELY, SSI 531180. REPLACED REINFORCEMENT PLATE LOCATED FWD PAX CABIN ENTRY DOOR L1 AT FR 20Oct 30, 2014 · N338NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2016112309187Floor Support · corrodedCORROSION ON BEAM AT AFT CARGO BAY BETWEEN FRAMES 58 TO 59 STRINGER 44. REMOVED AND REPLACED THE BEAM.Oct 28, 2014 · N338NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2014102905822Structure · corrodedDURING INSPECTION, FOUND CORROSION ON UPPER INTERNAL CUTOUT OF TAIL COMPARTMENT ACCESS DOOR AT FRAME 72. REPLACED INTERNAL DOUBLER CUTOUT IAW SRM 51-72-11 AND DWG D53571511, D53571510.Oct 28, 2014 · N338NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014102905821Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 42L, BETWEEN FRAMES 56 - 57 IN THE AFT CARGO BAY. REPAIRED THE STRINGER IAW SRM 53-00-13, PARA 4.A, 7, FIG 201, SHEET 2, PAG 211/212.Oct 28, 2014 · N338NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2014102905820Skin · dentedDURING INSPECTION, FOUND A DENT ON THE SKIN OF THE LT AFT PASSENGER DOOR LOWER EDGE. REPAIRED IAW SRM 52-10-00; PARA 5.C, FIG 203.Oct 28, 2014 · N338NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2014102905819Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT IN AFT PAX CABIN BETWEEN FRAMES 66 - 68 STRINGER 23L. REPLACED IAW SRM 51-72-11 AND DWG D53480505.Oct 28, 2014 · N338NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014102905818Skin · damagedDURING INSPECTION, FOUND BENT ON EXTERNAL PLATE OF THE LT FORWARD PASSENGER/ CREW DOOR UPPER EDGE. REPLACED EXTERNAL PLATE OF THE LT FORWARD PASSENGER/CREW DOOR UPPER EDGE IAW SRM 51-72-11 AND DWG D52110475.Oct 27, 2014 · N338NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2014102805788Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB IN THE AFT CARGO BAY BETWEEN FRAMES 62-63, STRINGER 38L. REPLACED THE WEB IAW SRM 51-72-11 AND DWG D53470320.Oct 27, 2014 · N338NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014102805787Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON FRAME 64 SHEAR TIE BETWEEN STRINGERS 43-44R. REPLACED THE SHEAR TIE IAW SRM 51-72-11 AND DWG D53470342; D53470330.Oct 27, 2014 · N338NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2014102805786Profile · crackedDURING INSPECTION, FOUND CRACK ON LT LOAD TRANSMITTING PROFILE OF THE EMERGENCY EXIT . REPLACED PROFILE IAW SRM 51-72-11 AND DWG D52279040.Oct 27, 2014 · N338NW · Airbus A320212 · Emergency ExitsSDR DALA2014102805785Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 16 - 20, Y-254. REPLACED THE FLOOR SUPPORT IAW PR1 528840-14, REV 0, ERA 528840-14, REV ORIGINAL AND SRM 51-72-11.Oct 27, 2014 · N338NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014102805784Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 25L FRAME 67. REPLACED SECTION OF STRINGER IAW PR1 529839-14, REV 0, ERA 5298-39-14 REV ORIGINAL AND SRM 51-72-11.Oct 27, 2014 · N338NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2014102705780Door Frame · crackedDURING INSPECTION, FOUND A CRACK ON RT VERTICAL FRAME LOWER POSITION IN EMERGENCY EXIT. REPLACED RT VERTICAL FRAME LOWER POSITION IN EMERGENCY EXIT 834 IAW SRM 51-72-11, DWS D52279040 AND D52279010.Oct 26, 2014 · N338NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2014102705779Door Sill · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER DOOR SILL BETWEEN FRAMES 66-68. REPLACED THE DOOR SILL IAW SRM 51-72-11 AND DWG D53480505.Oct 26, 2014 · N338NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014102705778Seat Track · corrodedSEAT TRACK BETWEEN FRAMES 47-64 AND Y1292, FOUND CORRODED OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53472000.Oct 26, 2014 · N338NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014102705777Door Sill · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER L1 DOOR SILL, FRAME 20. STRINGER 23L. REPLACED THE DOOR SILL IAW SRM 51-72-11 AND DWG.Oct 26, 2014 · N338NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014102705776Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR TIE FRAME 30, BETWEEN STRINGERS 40 - 41L. REPLACED THE SHEAR TIE IAW SRM 51-72-11, DWG D532-30320 AND D532-31212.Oct 26, 2014 · N338NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2014102605774Skin · dentedDURING INSPECTION, FOUND A DENT ON EXTERNAL SKIN BETWEEN FRAMES 24A - 25 STRINGERS 43L-STR 43R, LOWER FUSELAGE. REPAIRED IAW SRM 53-00-11.Oct 25, 2014 · N338NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2014102605773Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 31R BETWEEN FRAMES 65 - 66. REPLACED THE STRINGER IAW SRM 51-72-11.Oct 25, 2014 · N338NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2014102605772Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 42L BETWEEN FRAMES 56 - 57. REPAIRED THE STRINGER IAW SRM 53-00-13, PARA 4.A, 7, FIG 201, SHEET 2, PAG 211/212.Oct 25, 2014 · N338NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2014102605771Profile · crackedDURING INSPECTION, FOUND CRACK ON RT LOAD TRANSMITTING PROFILE IN EMERGENCY EXIT. REPLACED IAW SRM 51-72-11 AND DWG D52279010.Oct 25, 2014 · N338NW · Airbus A320212 · Emergency ExitsSDR DALA2014102505770Profile · crackedDURING INSPECTION, FOUND CRACK ON RT LOAD TRANSMITTING PROFILE OF THE EMERGENCY EXIT. REPLACED THE PROFILE IAW SRM 51-72-11 AND DWG D522-79010 .Oct 24, 2014 · N338NW · Airbus A320212 · Emergency ExitsSDR DALA2014102505769Door Frame · crackedDURING INSPECTION, FOUND CRACK ON RT VERTICAL FRAME UPPER POSITION IN EMERGENCY EXIT 844, SSI 522102-01-1. REPLACED SEGMENT FRAME UPPER POSITION IN EMERGENCY EXIT DOOR 844 IAW SRM A320 51-72-11 AND DWG D52279010.Oct 24, 2014 · N338NW · Airbus A320212 · Emergency ExitsSDR DALA2014102505768Profile · crackedDURING INSPECTION, FOUND CRACK ON RT LOAD TRANSMITTING PROFILE IN EMERGENCY EXIT 844, SSI 522102-01-1. REPLACED SEGMENT ANGLE LOCATED IN EMERGENCY EXIT 844 IAW SRM 51-72-11 AND DWG D52279010.Oct 24, 2014 · N338NW · Airbus A320212 · Emergency ExitsSDR DALA2014102505767Door Frame · crackedDURING INSPECTION, FOUND CRACK ON RT VERTICAL FRAME UPPER POSITION IN EMERGENCY EXIT 843. REPLACED RT VERTICAL FRAME UPPER POSITION IN EMERGENCY EXIT 843 IAW SRM 51-72-11 AND DWG D52279010.Oct 24, 2014 · N338NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2014102505766Profile · crackedDURING INSPECTION, FOUND CRACK ON RT LOAD TRANSMITTING PROFILE IN EMERGENCY EXIT 843. REPLACED LOAD TRANSMITTING PROFILE IN EMERGENCY EXIT 843 IAW SRM 51-72-11 AND DWG D52279010.Oct 24, 2014 · N338NW · Airbus A320212 · Emergency ExitsSDR DALA2014102505765Structure · corrodedDURING INSPECTION, FOUND CORROSION ON AFT LOWER CORNER AT FRAME 20. LEFT OF FWD PASSENGER DOOR CUTOUT. REPLACED LOWER CORNER AND FASTENERS LOCATED FRAME 20 ON LOWER SILL L1 IAW SRM 51-72-11 AND DWG D531-12109.Oct 24, 2014 · N338NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2014102405737Seat Track · corrodedSEAT TRACK BETWEEN FRAMES 47-64, Y1292 CORRODED OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53472000.Oct 23, 2014 · N338NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014102405736Support Angle · corrodedDURING INSPECTION, FOUND CORROSION ON SUPPORT ANGLE IN EMERGENCY EXIT 833 AT AFT VERTICAL FRAME. REPLACED THE SUPPORT ANGLE IAW SRM 51-72-11 AND DWG D522-79040.Oct 23, 2014 · N338NW · Airbus A320212 · Emergency ExitsSDR DALA2014102405735Support Angle · corrodedDURING INSPECTION, FOUND CORROSION ON SUPPORT ANGLE IN EMERGENCY EXIT 833 AT FORWARD VERTICAL FRAME. REPLACED SUPPORT ANGLE IAW SRM 51-72-11 AND DWG D522-79040.Oct 23, 2014 · N338NW · Airbus A320212 · Emergency ExitsSDR DALA2014102405734Support · corrodedDURING INSPECTION, FOUND CORROSION ON LT SUPPORT ANGLE IN EMERGENCY EXIT 844 LOWER POSITION. REPLACED THE SUPPORT IAW SRM 51-72-11 AND DWG D52279010.Oct 23, 2014 · N338NW · Airbus A320212 · Emergency ExitsSDR DALA2014102405733Seat Track · corrodedSEAT TRACK BETWEEN FRAMES 41-47 -Y765 FOUND CORRODED OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53370500;Oct 23, 2014 · N338NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014102405732Seat Track · corrodedSEAT TRACK LOCATED BETWEEN FRAMES 36-41, Y765 FOUND CORRODED OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D57130146.Oct 23, 2014 · N338NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014102305730Stringer Splice · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER SPLICE 43L BETWEEN FRAMES 30 AND 31. REPLACED THE STRINGER SPLICE IAW SRM 51-72-11 AND DWG D53231375.Oct 22, 2014 · N338NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2014102305729Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1162 BETWEEN FRAMES 67+15 AND 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Oct 22, 2014 · N338NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014102205697Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 41L BETWEEN FRAMES 33 - 34 . REPLACED THE STRINGER IAW SRM 51-72-11 AND DWG 53231626.Oct 21, 2014 · N338NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2014102205696Seat Track · corrodedSEAT TRACK LOCATED BETWEEN FRAMES 47 - 64, Y765 FOUND OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53472000.Oct 21, 2014 · N338NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014102205695Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1225 BETWEEN FRAMES 66+5 - 67+15. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG, D53470150 AND DWG D53472831.Oct 21, 2014 · N338NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014102105675Seat Track · corrodedSEAT TRACK BETWEEN FRAMES 36-41, Y1292 FOUND CORRODED OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11V AND DWG D53370500.Oct 20, 2014 · N338NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014102105676Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON THE SHEAR TIE OF FRAME 31 BETWEEN STRINGERS 43 - 44L. REPLACED THE SHEAR TIE IAW SRM 51-72-11 AND DWG D53230811.Oct 20, 2014 · N338NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2014102105674Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON THE SHEAR TIE OF FRAME 31 BETWEEN STRINGERS 40 - 41L. REPLACED THE SHEAR TIE IAW 51-72-11 AND DWG D53231212.Oct 20, 2014 · N338NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2014102105673Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR TIE AT FRAME 30 AND BETWEEN STRINGERS 43 - 44L. REPLACED THE SHEAR TIE IAW SRM 51-72-11 AND DWG D53231212.Oct 20, 2014 · N338NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2014102105672Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR TIE AT FRAME 30 AND BETWEEN STRINGERS 42-43L. REPLACED THE SHEAR TIE IAW SRM 51-72-11 AND DWG D53231212.Oct 20, 2014 · N338NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2014102105671Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR TIE OF FRAME 32 BETWEEN STRINGERS 40 AND 41L. REPLACED THE SHEAR TIE IAW SRM 51-72-11 AND DWG D53231212.Oct 20, 2014 · N338NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2014102005635Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR TIE OF FRAME 32 BETWEEN STRINGERS 42 - 43L. REPLACED THE SHEAR TIE IAW SRM 51-72-11 AND DWG D53230811.Oct 19, 2014 · N338NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2014102005634Stringer Splice · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER SPLICE 41R BETWEEN FRAMES 30 - 31. REPLACED THE STRINGER SPLICE IAW SRM 51-72-11 AND DWG D53231586.Oct 19, 2014 · N338NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2014102005633Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON A FLOOR SUPPORT BETWEEN FRAMES 20 - 21, Y-189. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112834.Oct 19, 2014 · N338NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014102005632Seat Track · corrodedSEAT TRACK BETWEEN FRAMES 41 - 47, Y765 FOUND CORRODED OUT OF LIMITS. . REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53370500.Oct 19, 2014 · N338NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
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